forked from Archive/PX4-Autopilot
uORB: Moved tecs_status to generated topics
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uint8 TECS_MODE_NORMAL = 0
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uint8 TECS_MODE_UNDERSPEED = 1
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uint8 TECS_MODE_TAKEOFF = 2
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uint8 TECS_MODE_LAND = 3
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uint8 TECS_MODE_LAND_THROTTLELIM = 4
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uint8 TECS_MODE_BAD_DESCENT = 5
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uint8 TECS_MODE_CLIMBOUT = 6
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uint64 timestamp # timestamp, in microseconds since system start */
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float32 altitudeSp
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float32 altitude_filtered
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float32 flightPathAngleSp
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float32 flightPathAngle
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float32 flightPathAngleFiltered
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float32 airspeedSp
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float32 airspeed_filtered
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float32 airspeedDerivativeSp
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float32 airspeedDerivative
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float32 totalEnergyRateSp
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float32 totalEnergyRate
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float32 energyDistributionRateSp
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float32 energyDistributionRate
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uint8 mode
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@ -1,94 +0,0 @@
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/****************************************************************************
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*
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* Copyright (c) 2012-2014 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file vehicle_global_position.h
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* Definition of the global fused WGS84 position uORB topic.
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*
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* @author Thomas Gubler <thomasgubler@student.ethz.ch>
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*/
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#ifndef TECS_STATUS_T_H_
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#define TECS_STATUS_T_H_
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#include <stdint.h>
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#include <stdbool.h>
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#include "../uORB.h"
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/**
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* @addtogroup topics
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* @{
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*/
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typedef enum {
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TECS_MODE_NORMAL = 0,
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TECS_MODE_UNDERSPEED,
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TECS_MODE_TAKEOFF,
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TECS_MODE_LAND,
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TECS_MODE_LAND_THROTTLELIM,
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TECS_MODE_BAD_DESCENT,
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TECS_MODE_CLIMBOUT
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} tecs_mode;
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/**
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* Internal values of the (m)TECS fixed wing speed alnd altitude control system
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*/
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struct tecs_status_s {
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uint64_t timestamp; /**< timestamp, in microseconds since system start */
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float altitudeSp;
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float altitude_filtered;
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float flightPathAngleSp;
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float flightPathAngle;
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float flightPathAngleFiltered;
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float airspeedSp;
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float airspeed_filtered;
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float airspeedDerivativeSp;
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float airspeedDerivative;
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float totalEnergyRateSp;
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float totalEnergyRate;
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float energyDistributionRateSp;
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float energyDistributionRate;
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tecs_mode mode;
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};
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/**
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* @}
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*/
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/* register this as object request broker structure */
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ORB_DECLARE(tecs_status);
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#endif
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